Aerodynamic characteristics in sideslip of wing-fuselage combinations; wings have sweep angle of 45° at quarter-chord line, aspect ratio of 4, taper ratios of 0.3, 0.6, and 1.0, and NACA 65A006 airfoil section.


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    Title :

    Wind-tunnel investigation of static lateral stability characteristics of wing-fuselage combinations at high subsonic speeds -- Taper-ratio series


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1957


    Size :

    25 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :